JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2009FA0000092Bearing · failedSPOOL BEARING ASSY FAILED INTERNALLY. BEARING ASSY NO LONGER ROTATES. THE UPPER BEARING LOWER SHIELD AND RETAINER HAS COME OFF, BEARING BALLS ARE LOOSE. THE LWR BEARING IS INTACT BUT NO LONGER ROTATES. (K)SDR 2008UALA06485Engine · malfunctionedSTRONG ODOR - OIL SMELL ON TAKEOFF DISSIPATED ON CLIMBOUT. REPLACED NR 2 ENGINE.SDR FDEA200811084795Engine · overtempAFTER 2 HOURS INTO FLT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUES AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CKLIST. EGT STILL FLUCTUATING WILDLY SO PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILL SDR 08FDEA04795Engine · malfunctionedAT 2 00 INTO FLIGHT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUE S AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CHECKLIST EGT STILL FLUCTUATING WILDLY SO WE PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILLSDR 2008FA0000750Stiffener · separatedWHILE UNDERGOING A CHECK 3 MAINT INSP DURING EARLY NOVEMBER 2008, THE STIFFENING RING ON THE 1ST LOW PRESSURE TURBINE NOZZLE ON ENGINE WAS FOUND SEPARATED AND TRAPPED BETWEEN THE 1ST LP TURBINE NOZZLE AND THE HIGH PRESSURE TURBINE NOZZLE. NO SECONDARY DAMAGE SDR DLM8K081492Engine · odorIMMEDIATELY UPON ROTATION, ALL F/A STATION AND COCKPIT SMELLED A VERY ACRID, HEAVY ODOR. APU WAS OFF A/C FLIGHT RETURNED TO LAND THERE WAS NO SMOKE PRESENT. MTC IN PROGRESS. FOUND LT ENGINE AS SOURCE OF ODOR. REMOVED AND REPLACED NR 1 PER TRANSMITTAL. CHESDR ASAA0853755Engine · malfunctionedGE REMOTE DIAGNOSTICS NR 1 ENGINE TREND DATA CONTINUES TO SHOW A GREATER THAN NORMAL EGT MARGIN LOSS. PRIORITY 2 NOTE ETOPS SIGNIFICANT. COMPLETED GAS PATH CLEANING PROCEDURE FOR NR 1 ENG THROUGH STEPS 25 OF AMM 72-00-00-100-804-F00.7. 85034, 30NOV08 ACCOMPLSDR CA081125007Engine · vibration(CAN) AT FL100 IN STEADY STATE, THE PILOT HEARD A STRONG NOISE COMING FROM THE ENG AND THE INSTRUMENTS INDICATED TEMP AT 800°C, NG AT 100 PERCENT AND TORQUE AT 2000 FT-LB. THE POWER LEVER WAS RETARDED AND PARAMETERS CAME BACK TO (NORMAL). THE FLIGHT CONTINUEDSDR UHLA2008110700003Engine · malfunctionedFLIGHT 5952 ATL-HPN ON FINAL APPROACH WITH GEAR DOWN AND FLAPS AT NR 5 POS, NR 2 ENG SPOOLED UP TO 80% UN-COMMANDED. CREW SHOT MISSED APPROACH. ON SECOND APPROACH AND SAME THING HAPPENED. CREW SHUT DOWN ENGINE. CREW DID NOT RECEIVE ANY MESSAGES IN AIR OR ON GRSDR CNMA20080010Engine · malfunctionedNR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT TOP OF CLIMB (29,000) INTERMITTENTLY. LIGHT BECAME SOLID AFTER 3 MINUTES. ENGINE SHUTDOWN IN FLIGHT IAW QRH PROCEDURE 4-1-2-19 AND CORRESPONDING CHECKLISTS. COMPLETED WORTAN 08-0368 R&R NR 2 ENGINE OIL STRASDR CA081105009Engine · flamed out(CAN) DURING CRUISE AT FL270, THE PILOT NOTICED A POWER ROLL BACK ON NR 2 ENGINE. HE IMMEDIATELY DIVERTED THE ACFT TO AN ALTERNATE AIRPORT. THE ENGINE THEN FLAMED OUT AND THE PILOT MADE A SINGLE ENGINE LANDING. THE FUEL CONTROL WAS REPLACED AND THE ACFT RELSDR UPS08M53826Engine · overtempAT 2600FT NR 2 ENGINE EGT CLIMBED TO 668 DEGREES FOR 30 SECONDS. VIBRATION FELT IN THE AIRFRAME. PERFORMED ENG OPERATIONAL OVERLIMITS INSPECTION AFTER EGT OVERTEMP IAW AMM 70-00-04-6-2. NO PHYSICAL DAMAGE NOTED. RAN ENGINE AT FLIGHT IDLE, ALL PATAMETERS CHECSDR CA081112009Engine · failed(CAN) DURING CRUISE AT FL180, THE CREW FELT A STRONG JOLT AND VIBRATIONS THROUGH THE AIRFRAME. A QUICK REVIEW OF THE GAGES SHOWED A POWER LOSS ON NR 2 ENG. THE ENG WAS SECURED AND THE CREW PERFORMED A SINGLE ENGINE LANDING. GROUND INSP FOUND NOTHING OF SIGNIFSDR CA081112007Engine · making metal(CAN) DURING FLIGHT, THE ENGINE LOST TORQUE AND OIL PRESSURE. THE PILOT SHUT IT DOWN AND PERFORMED A SINGLE ENGINE LANDING. POST FLIGHT INSPECTION FOUND THE PROPELLER SEIZED AND METAL DEBRIS IN THE EXHAUST. MANUFACTURER WILL CONTINUE INVESTIGATING THE EVENTSDR V2JA145103108Engine · power lossCREW NOTICED LOSS OF TORQUE AND OIL PRESSURE ON LT ENGINE. OIL PRESSURE LIGHT CAME ON. PER MANUAL, CREW CONTINUED WITH SECURING PROCEDURES AND SHUT DOWN LT ENGINE. AIRCRAFT LANDED WITH NO INCIDENT.SDR DL76P081475Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE. REPLACED NR 1 ENG PER TRANS 1T148AD.SDR DL76L081474Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE.SDR DL76L081473Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE.SDR DL76L081472Engine · defectiveENG FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENG. REPLACED NR 1 ENGINE PER TRANS 1T148.SDR CA081105007Engine · making metal(CAN) DURING FLIGHT TEST, THE ENG HAD A PARTIAL FEATHERING OF THE PROPELLER LEADING TO A PARTIAL LOST OF THRUST. THE ENGINE "CHIP LIGHT" CAME APPROX 20 SECONDS AFTER LOST OF THRUST. THE PILOT REDUCED POWER TO FLIGHT IDLE AND RETURNED TO BASE. POST FLIGHT INSP SDR USAA920081989Eec · failedFLT NR 245 BWI-PHX EMERGENCY LANDING CREW REPORTED LOSS OF POWER EXPERIENCED ON NR 2 ENGINE SEVERAL TIMES. ECAM INDICATED ENG 2 STALL. THERE WAS NO ASSOCIATED NOISE OR FAILURE. CREW DECLARED AN EMERGENCY AND RETURNED TO BWI LANDING WITHOUT INCIDENT. ECAM ISDR IXXA080029OEngine · flamed outAFTER LEVEL OFF AT 37,000 FT DURING THROTTLE REDUCTION NUMBER THREE ENGINE FLAMED OUT. THE CREW PERFORMED INFLIGHT START AT 22,000 FT, RESTART NORMAL. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CFM FAULT 51, TROUBLESHOT TREE, CLSDR CA081105006Engine · malfunctioned(CAN) DURING CLIMB SHORTLY AFTER T/O, THE NR 2 ENGINE HAD AN UNCOMMANDED AUTOFEATHER AND SUBSEQUENT OVERTORQUE. THE CREW SHUT THE ENGINE DOWN AND THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. TROUBLESHOSDR 2008UALA06308Engine · oil consumptionHIGH OIL CONSUMPTION.SDR 2008UALA06305Engine · unknownIDLE DISAGREE: IN AIR MODE LEFT ENG WILL ONLY MATCH RIGHT ENG WITH FLAPS AT 25 AND-OR ENG TAI SW ON.SDR 2008UALA06295Engine · fireNR 1 ENG - FIRE IN TAIL PIPE AFTER SHUTDOWN. SUSPECT OIL LEAK.SDR USAA EMB08018Engine · contaminatedFLIGHT 1711, CLT-ORF - APPROXIMATELY 100 FEET AFTER TAKEOFF THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT THERE WAS SMOKE/FUMES IN THE AFT GALLEY. THE CAPTAIN REQUESTED TO RETURN TO CLT AND THE EMERGENCY EQUIPMENT STAND BY. THE CAPTAIN STATED THE SMOKE AND SDR TIMA20080006Engine · seizedPILOT FELT A POWER SURGE AND SAW FLAMES OUT THE LEFT ENGINE EXHAUST FOR A MOMENT. LEFT PROPELLER STOPPED TURNING. PILOT SECURED ENGINE, CONTINUED ON AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE PT BLADES WERE MOSTLY GONE. CT BLADES ARE OK. SDR COMA0870028Engine · vibrationLT ENGINE N2 VIB ON CLIMBOUT FROM CVG. ACFT RETURNED TO CVG. LANDED SAFELY. R&R LT ENGINE.SDR 2008UALA06270Blade · damagedNUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES.SDR DXTA2008102703321Engine · unknownLT & RT ENGINE FAILED TO DEVELOP TAKEOFF THRUST. PERFORMED MULTIPLE ENGINE RUNS. ADJUSTED EFC AUTHORITY ON LT ENGINE AND CHECKED ALL RIGGING AND PARAMETERS. AT OAT 10 DEGREE C DESIRED THRUST OF 98-0 BOTH ENGINES PRODUCED 99-0. IAW MM AND MFG REF, BOTH ENGINESDR DL76P081462Engine · failedOIL LOSS IN FLIGHT AND IFSD. REPLACED RT ENG PER TRANSMITTAL 1T149AD9.SDR DL75E081447Engine · malfunctionedREJECTED TAKEOFF RWY 13R KJFK FOR LOSS OFF EPR INDICATION LEFT ENG ALL OTHER INDICATIONS NORMAL. RTO INITIATED 50 KTS GS, LOW SPEED REJECT. CONSULTED W/JFK MTC DISPATCH. RESTARTED ENG ALL INDICATIONS NORMAL. EPCS MSGS NR 1 ENG P2 RESET ALSO S DCI DC2 EPR SDR DLM90081435Engine · bird ingestionHIT BIRD AT ABOUT 135 KTS. HIGH SPEED ABORT ACCOMPLISHED AND PARKED WITH HOT BRAKES. RT ENGINE FLUCTUATED AND HAD NOTICABLE POWER LOSS WITH THE BIRD STRIKE. BRAKE TEMP REACHED 650. REPLACED NR 2 ENGINE.SDR 22AA20081004Engine · malfunctionedAFTER TAKEOFF HEARD LOUD NOISE. TOWER ADVISED, FLAMES COMING FROM AIRCRAFT AND NR 1 ENGINE EGT WENT TO RED LINE. ENGINE SHUTDOWN ON ITS OWN. ENGINE CHANGE IN PROGRESS.
SDR DLM88081664Bolt · wornWEAR ON AFT CONE BOLT FLANGES (BOTH SIDES) ON RT ENGINE. WEAR REWORKED IAW EA 49-469467-14 REV ORIG. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL.SDR DL76L081430Engine · malfunctionedAFTER LEVEL OFF AT FL 364 THE LEFT ENGINE SPOOLED BACK ON ITS OWN FOLLOWED BY NUMEROUS EEC AND ENGINE OUT MESSAGES. T/S PER FIM INSPECTION FUEL SAMPLES PLUS NR 1 ENG FUEL FILTER FOR CONTAMINATION. FILTER PLUS FUEL SAMPLE FOUND CLEAN C/W ENG FU SUCTION FEED OSDR C2XA08TY127Flange · corrodedACFT WAS IN FOR A 3C INSPECTION AND THE NR 1 ENGINE FORWARD BOLT FLANGE WAS FOUND CORRODED. 2 BOLT HOLES AT NR 29 AND NR 45 WERE FOUND IF REPAIRED WOULD RESULT IN BEING BEYOND THE MM LIMITS AND REPAIR OF THE HOLES WOULD RESULT IN A THINWALL CONDITION. ALL OTSDR SIMA200830102Engine · malfunctionedFLIGHT 4292 - ON CLIMBOUT CREW OBSERVED SMOKE IN THE CABIN AND COCKPIT. CREW ELECTED TO RETURN TO CMH. AIRCRAFT LANDED AND TAXIED SAFELY TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE IAW WORK CASDR YENA200810240101Engine · bird ingestionJFK-PIT, STRONG UNKNOWN FUMES IN COCKPIT AND CABIN DURING INITIAL CLIMB. COMPLETED CABIN /SMOKE FUMES QRH AND RETURNED TO JFK. FUMES DISSIPATED INFLIGHT PRIOR TO LANDING. ACCOMPLISHED FIM TASK 21-20-00-810-801-A SMOKE AND /OR ABNORMAL SMELL IN PASSENGER CABSDR DXTA2008102403315Engine · shutdownENG NR 1 SHUT DOWN BY FADEC (LOW OIL PRESS FLICKERED ON).SDR DL76L081625Engine · failedNR 2 ENGINE FAILED 25 CYCLE RE-INSPECT OF GEARBOX FOR BLAST CONTAMINANT. REPLACED NR 2 ENGINE.SDR UALA2008111306192Engine · stalledTWO ENGINES STALLED AT FL380. DFDR INVESTIGATION REVEALED THAT ONLY THE NUMBER 2 ENGINE STALLED. AIRPLANE ENCOUNTERED AN ATMOSPHERIC WAVE AT .80 MACH CAUSING AUDIBLE COMPRESSOR STALLS AND A FLUCTUATION IN THE MACH METER FROM .75 TO .84 RETURNING TO .80. CRESDR 2008UALA06192Engine · stalledTWO ENGINES STALLED AT FL380.SDR DL777081377Engine · inoperativeLEFT ENGINE START VALVE FAILED TO OPEN AFTER PUSHBACK. RTB AND APPLIED MEL AND PERFORMED A MANUAL START.SDR IXXA080026OEngine · flamed outDURING CLIMBOUT FROM KPDX AT 39000 FT NUMBER 4 ENGINE FLAMED OUT, AIRSPEED UNKNOWN, MACH .78, ALT 36.0, RAT UNKNOWN, WT 220.0 WEATHER CLEAR NO FIRE WARNING. GENERATOR WENT OFF LINE, OIL PRESS LIGHT ON, IGNITION OFF, FUEL FEED NOT CHANGED, WINDMILLING OIL PRESSDR DL738081370Engine · seizedDURING CRUISE AT FL 370 ENGINE SEIZED. BOTH N1 AND N2 RAPIDLY DECREASED TO ZERO. AUTOPILOT KICKED OFF AND SIGNIFICANT AILERON INPUT REQUIRED TO RETURN TO WINGS LEVEL. DIVERTED TO ORD. NO LOSS OF ENGINE OIL. NO PREVIOUS VIBRATIONS. NO WARNING OST FLIGHT CSDR FDEA200810154371Engine · failedNUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPROVSDR 08FDEA04371Engine · hung startNUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPSDR 2008UALA06096Engine · malfunctionedENG VIB MONITOR R RIGHT ENGINE AIRBORNE VIBRATION MONITORING (AVM) SYSTEM IS INOPERATIVE, OR LOSS OF TACHOMETER DATA. STATUS MSG01- NOT ACTIVE DESCENT INTERMITTENT; 'E' FLANGE ACCELEROMETER (CIRCUIT 1 RIGHT) SIGNAL IS OUT OF RANGE. DB- SIGNAL CONDITIONER UN
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